GB2053757A - Lost wax patterns - Google Patents

Lost wax patterns Download PDF

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Publication number
GB2053757A
GB2053757A GB7925125A GB7925125A GB2053757A GB 2053757 A GB2053757 A GB 2053757A GB 7925125 A GB7925125 A GB 7925125A GB 7925125 A GB7925125 A GB 7925125A GB 2053757 A GB2053757 A GB 2053757A
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GB
United Kingdom
Prior art keywords
wax
pattern
wax pattern
distortion
patterns
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
GB7925125A
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GB2053757B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB7925125A priority Critical patent/GB2053757B/en
Publication of GB2053757A publication Critical patent/GB2053757A/en
Application granted granted Critical
Publication of GB2053757B publication Critical patent/GB2053757B/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C7/00Patterns; Manufacture thereof so far as not provided for in other classes
    • B22C7/02Lost patterns

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

Means for reducing distortion in a wax pattern 10, e.g. for a gas turbine engine nozzle guide comprises moulding at least one wax supporting member 14 into the wax pattern which serves to support that portion 12,13 of the wax pattern liable to distortion. <IMAGE>

Description

SPECIFICATION Lost wax patterns This invention relates to wax patterns suitable for use in making castings by the lost wax process and more particularly to such patterns having an ability to resist distortion.
It is well known that it is possible by use of the lost wax process to manufacture castings to extremely close tolerances. This makes the process particularly suitable for producing large quantities of highly accurate castings for use in the manufacture of gas turbine engine components.
The process does however have disadvantages. In particular after the wax pattern has been injected it is removed from the die whilst it is still quite soft. This must be done to prevent the patterns cracking due to contraction of the wax and also to maintain an acceptable production rate. Certain wax patterns due to their relatively thin cross-section or complexity which are known to be susceptible to distortion are therefore placed in "setters" after injection where they are allowed to harden off. The setter is usually manufactured from plaster of paris and consists of a mould which conforms to the desired size and shape of the completed wax pattern.
Any distortion which occurs on the wax pattern after injection will therefore be eliminated by the setter. However it is usual to remove the wax pattern from the setter after approximately one hour so that the setter can be used to accommodate a further wax pattern. However the wax pattern after removal from the setter has a residual memory which remains for about one week, so therefore it is highly likely that the wax pattern will therefore distort again.
One way to overcome this problem is to allow the wax patterns to remain in the setters for a week.
However for mass-produced items this would necessitate an extremely large number of setters which would obviously prove expensive and would also create a considerable storage problem.
An object of the present invention is to provide wax patterns in which the aforementioned problems are substantially eliminated.
According to the present invention means for reducing distortion in parts of wax patterns comprises forming at least one wax supporting member upon the pattern during the wax injection stage, the at least one supporting member serving to restrain the parts of the wax pattern liable to distortion.
Preferably the at least one support can remain as a part of the pattern until after the casting has been made whereupon the excess metal formd by the at least one wax support member may be machined from the finished casting.
Alternatively the supports may be cut from the wax pattern prior to being used to form the ceramic mould for the casting.
For better understanding of the invention an embodiment thereof will be more particularly described by way of example only and with reference to the accompanying drawing in which there is shown a pictorial view of a wax pattern made in accordance with the present invention.
The drawing shows generally at 10 a pictorial view of a wax pattern suitable for manufacturing a gas turbine engine nozzle guide vane which comprises an aerofoil vane portion 11, and radially inner and outer platforms shown at 12 and 13 respectively. As can be seen from the drawing the platform portions 12 and 13 are relatively thin and weak and are obviously liable to distortion at their extremities. The platforms are therefore provided with supporting members 14, 15, 16 and 17 which are cast into the wax pattern during the wax injection stage.
In this example the supporting members 14, 15,16 and 17 are formed such as to simply extend between the two platforms 12 and 13. However in the case of the other shaped castings a supporting member or members may be located in any convenient location.
In certain circumstances it may be convenient to remove the supporting members just prior to the wax pattern being used for manufacturing the mould. In this way the wax pattern is supported for the maximum possible time without the necessity of using "setters". There is therefore little likelyhood of any distortion occurring in the brief time it takes to manufacture the mould from the wax pattern.
Alternatively the supporting members may be left as a portion of the wax pattern and therefore form a part of the resulting mould. It will therefore then be necessary to remove the supporting members from the completed casting by machining.
It will be appreciated that whilst the invention has been described as supporting members used for the manufacture of the nozzle guide vane for a gas turbine engine the scope of the invention is not restricted to such an application. The invention could equally well be utilised in the manufacture of any shape of casting produced by the lost wax process and in which the wax pattern is liable to distortion.
1. Means for reducing distortion in a part or parts of a wax pattern comprising forming at least one wax supporting member upon the pattern during the wax injection stage, the at least one supporting member serving to restrain the parts of the wax pattern liable to distortion.
2. Means for reducing distortion within a wax pattern as claimed in claim 1 in which the at least one support can remain as a part of the pattern until after the casting has been made, whereupon the excess metal formed by the at least one wax support member may be removed from the finished casting.
3. Means for reducing distortion within a wax pattern as claimed in claim 1 in which the at least one support may be cut from the wax pattern prior to it being used to form the ceramic mould for the casting.
4. Means for reducing distortion in a wax pattern as claimed in any preceding claim, substantially as hereinbefore described by way of example only and with reference to the accompanying drawings.
Printed for Her Majesty's Stationery Office by Croydon Printing Company Limited, Croydon Surrey, 19ûû.
Published bythe Patent Office, 25 Southampton Buildings, London, WC2A 1AY, from which copies may be obtained.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (4)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Lost wax patterns This invention relates to wax patterns suitable for use in making castings by the lost wax process and more particularly to such patterns having an ability to resist distortion. It is well known that it is possible by use of the lost wax process to manufacture castings to extremely close tolerances. This makes the process particularly suitable for producing large quantities of highly accurate castings for use in the manufacture of gas turbine engine components. The process does however have disadvantages. In particular after the wax pattern has been injected it is removed from the die whilst it is still quite soft. This must be done to prevent the patterns cracking due to contraction of the wax and also to maintain an acceptable production rate. Certain wax patterns due to their relatively thin cross-section or complexity which are known to be susceptible to distortion are therefore placed in "setters" after injection where they are allowed to harden off. The setter is usually manufactured from plaster of paris and consists of a mould which conforms to the desired size and shape of the completed wax pattern. Any distortion which occurs on the wax pattern after injection will therefore be eliminated by the setter. However it is usual to remove the wax pattern from the setter after approximately one hour so that the setter can be used to accommodate a further wax pattern. However the wax pattern after removal from the setter has a residual memory which remains for about one week, so therefore it is highly likely that the wax pattern will therefore distort again. One way to overcome this problem is to allow the wax patterns to remain in the setters for a week. However for mass-produced items this would necessitate an extremely large number of setters which would obviously prove expensive and would also create a considerable storage problem. An object of the present invention is to provide wax patterns in which the aforementioned problems are substantially eliminated. According to the present invention means for reducing distortion in parts of wax patterns comprises forming at least one wax supporting member upon the pattern during the wax injection stage, the at least one supporting member serving to restrain the parts of the wax pattern liable to distortion. Preferably the at least one support can remain as a part of the pattern until after the casting has been made whereupon the excess metal formd by the at least one wax support member may be machined from the finished casting. Alternatively the supports may be cut from the wax pattern prior to being used to form the ceramic mould for the casting. For better understanding of the invention an embodiment thereof will be more particularly described by way of example only and with reference to the accompanying drawing in which there is shown a pictorial view of a wax pattern made in accordance with the present invention. The drawing shows generally at 10 a pictorial view of a wax pattern suitable for manufacturing a gas turbine engine nozzle guide vane which comprises an aerofoil vane portion 11, and radially inner and outer platforms shown at 12 and 13 respectively. As can be seen from the drawing the platform portions 12 and 13 are relatively thin and weak and are obviously liable to distortion at their extremities. The platforms are therefore provided with supporting members 14, 15, 16 and 17 which are cast into the wax pattern during the wax injection stage. In this example the supporting members 14, 15,16 and 17 are formed such as to simply extend between the two platforms 12 and 13. However in the case of the other shaped castings a supporting member or members may be located in any convenient location. In certain circumstances it may be convenient to remove the supporting members just prior to the wax pattern being used for manufacturing the mould. In this way the wax pattern is supported for the maximum possible time without the necessity of using "setters". There is therefore little likelyhood of any distortion occurring in the brief time it takes to manufacture the mould from the wax pattern. Alternatively the supporting members may be left as a portion of the wax pattern and therefore form a part of the resulting mould. It will therefore then be necessary to remove the supporting members from the completed casting by machining. It will be appreciated that whilst the invention has been described as supporting members used for the manufacture of the nozzle guide vane for a gas turbine engine the scope of the invention is not restricted to such an application. The invention could equally well be utilised in the manufacture of any shape of casting produced by the lost wax process and in which the wax pattern is liable to distortion. CLAIMS
1. Means for reducing distortion in a part or parts of a wax pattern comprising forming at least one wax supporting member upon the pattern during the wax injection stage, the at least one supporting member serving to restrain the parts of the wax pattern liable to distortion.
2. Means for reducing distortion within a wax pattern as claimed in claim 1 in which the at least one support can remain as a part of the pattern until after the casting has been made, whereupon the excess metal formed by the at least one wax support member may be removed from the finished casting.
3. Means for reducing distortion within a wax pattern as claimed in claim 1 in which the at least one support may be cut from the wax pattern prior to it being used to form the ceramic mould for the casting.
4. Means for reducing distortion in a wax pattern as claimed in any preceding claim, substantially as hereinbefore described by way of example only and with reference to the accompanying drawings.
Printed for Her Majesty's Stationery Office by Croydon Printing Company Limited, Croydon Surrey, 19ûû.
Published bythe Patent Office, 25 Southampton Buildings, London, WC2A 1AY, from which copies may be obtained.
GB7925125A 1979-07-19 1979-07-19 Lost wax patterns Expired GB2053757B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7925125A GB2053757B (en) 1979-07-19 1979-07-19 Lost wax patterns

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7925125A GB2053757B (en) 1979-07-19 1979-07-19 Lost wax patterns

Publications (2)

Publication Number Publication Date
GB2053757A true GB2053757A (en) 1981-02-11
GB2053757B GB2053757B (en) 1983-02-23

Family

ID=10506596

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7925125A Expired GB2053757B (en) 1979-07-19 1979-07-19 Lost wax patterns

Country Status (1)

Country Link
GB (1) GB2053757B (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0084234A1 (en) * 1981-12-16 1983-07-27 Vickers Plc Investment casting process and mould
US5014763A (en) * 1988-11-30 1991-05-14 Howmet Corporation Method of making ceramic cores
US5126082A (en) * 1988-11-30 1992-06-30 Howmet Corporation Method of making ceramic cores and other articles
EP2241391A1 (en) * 2009-04-14 2010-10-20 Siemens Aktiengesellschaft Method for producing a negative mould for casting a turbine rotor and mould for producing a wax model of a turbine rotor
FR3076752A1 (en) * 2018-01-15 2019-07-19 Safran Aircraft Engines METHOD FOR MAKING A MULTI-PALE MODEL, TOOLING AND ASSEMBLY OF A MULTI-PALE MODEL AND A HOLDING ELEMENT
CN113664147A (en) * 2021-08-02 2021-11-19 安徽应流航源动力科技有限公司 Blade wax pattern wax-spraying 3D printing deformation prevention process
CN114523070A (en) * 2022-03-01 2022-05-24 中国航发北京航空材料研究院 Deformation prevention control method for crown turbine blade casting

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0084234A1 (en) * 1981-12-16 1983-07-27 Vickers Plc Investment casting process and mould
US5014763A (en) * 1988-11-30 1991-05-14 Howmet Corporation Method of making ceramic cores
US5126082A (en) * 1988-11-30 1992-06-30 Howmet Corporation Method of making ceramic cores and other articles
EP2241391A1 (en) * 2009-04-14 2010-10-20 Siemens Aktiengesellschaft Method for producing a negative mould for casting a turbine rotor and mould for producing a wax model of a turbine rotor
WO2010118960A1 (en) * 2009-04-14 2010-10-21 Siemens Aktiengesellschaft Method for producing a negative mold for casting a turbine blade and mold for producing a wax model of a turbine blade
FR3076752A1 (en) * 2018-01-15 2019-07-19 Safran Aircraft Engines METHOD FOR MAKING A MULTI-PALE MODEL, TOOLING AND ASSEMBLY OF A MULTI-PALE MODEL AND A HOLDING ELEMENT
US10682685B2 (en) 2018-01-15 2020-06-16 Safran Aircraft Engines Method of making a multi-vane model, tooling, and an assembly comprising a multi-vane model and a holder element
CN113664147A (en) * 2021-08-02 2021-11-19 安徽应流航源动力科技有限公司 Blade wax pattern wax-spraying 3D printing deformation prevention process
CN113664147B (en) * 2021-08-02 2023-10-20 安徽应流航源动力科技有限公司 Anti-deformation process for wax spraying and 3D printing of blade wax mould
CN114523070A (en) * 2022-03-01 2022-05-24 中国航发北京航空材料研究院 Deformation prevention control method for crown turbine blade casting
CN114523070B (en) * 2022-03-01 2022-12-16 中国航发北京航空材料研究院 Deformation prevention control method for casting shrouded turbine blade

Also Published As

Publication number Publication date
GB2053757B (en) 1983-02-23

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930719